View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 65474U 26145.03320338 +.00000000 +00000-0 +64768-3 0 00003
2 65474 53.1590 263.4700 0002520 76.8431 283.2851 15.30213130 09
| Epoch (UTC): | 25 May 2026 00:47:48 |
| Eccentricity: | 0.0002520 |
| inclination: | 53.1590° |
| perigee height: | 473 km |
| apogee height: | 477 km |
| right ascension of ascending node: | 263.4700° |
| argument of perigee: | 76.8431° |
| revolutions per day: | 15.30213130 |
| mean anomaly at epoch: | 283.2851° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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